Mayle, R. E., 1991, “The Role of Laminar-Turbulent Transition in Gas Turbine Engines,” ASME J. Turbomach., 113 , pp. 509–537.

Lakshminarayana, B., 1991, “An Assessment of Computational Fluid Dynamic Techniques in the Analysis and Design of Turbomachinery—The 1990 Freeman Scholar Lecture,” ASME J. Fluids Eng., 113 , pp. 315–352.

Simoneau, R. J., and Simon, F. F., 1993, “Progress Towards Understanding and Predicting Heat Transfer in the Turbine Gas Path,” Int. J. Heat Fluid Flow

[CrossRef], 14 , pp. 106–128.

Simon, F. F., and Ashpis, D. E., 1996, “Progress in Modeling of Laminar to Turbulent Transition on Turbine Vanes and Blades,” NASA Technical Memorandum No. 107180.

Dunn, M. G., 2001, “Convective Heat Transfer and Aerodynamics in Axial Flow Turbines,” ASME Paper No. 2001-GT-0506.

Yaras, M. I., 2002, “Measurements of the Effects of Freestream Turbulence on Separation-Bubble Transition,” ASME Paper No. GT-2002–30232.

Wilcox, D. C., 1998, "*Turbulence Modeling for CFD*", 2nd ed., DCW Industries, Inc., La Canada, CA.

Ames, F. E., 1994, “Experimental Study of Vane Heat Transfer and Aerodynamics in Elevated Levels of Turbulence,” NASA Contract Report No. 4633.

Ni, R. H., 1999, “Advanced Modeling Techniques for New Commercial Engines,” 1999, *Proceedings of the XIV International Symposium on Air Breathing Engines* , Florence, Italy, 5–10 September.

Davis, R. L., Shang, T., Buteau, J., and Ni, R. H., 1996, “Prediction of 3-D Unsteady Flow in Multi-Stage Turbomachinery Using an Implicit Dual Time-Step Approach,” AIAA Paper No. 96–2565.

Abu-Ghannam, B. J., and Shaw, R., 1980, “Natural Transition of Boundary Layers—The Effects of Turbulence, Pressure Gradient, and Flow History,” J. Mech. Eng. Sci., 22 (5), pp. 213–228.

Wilcox, D. C., 1988, “Reassessment of the Scale-Determining Equation for Advanced Turbulence Models,” AIAA J., 26 , pp. 1299–1310.

Baines, W. D., and Peterson, E. G., 1951, “An Investigation of Flow Through Screens,” Trans. ASME, 73 , pp. 467–480.

Hinze, J. O., 1975, Turbulence , 2nd ed., McGraw–Hill, New York, p. 272.

Ames, F. E., and Plesniak, M. W., 1995, “The Influence of Large Scale, High Intensity Turbulence on Vane Aerodynamic Losses, Wake Growth, and Exit Turbulence Parameters,” ASME Report No. 95-GT-290.

Moss, R. W., and Oldfield, M. L. G., 1992, “Measurements of the Effect of Free-Stream Turbulence Length Scale on Heat Transfer,” ASME Report No. 92-GT-244.

Boyle, R. J., Bunker, R. S., and Giel, P. W., 2003, “Predictions for the Effects of Turbulence on Turbine Blade Heat Transfer,” ISABE Report No. 2003 1178.

Roach, P. E., and Brierley, D. H., 2000, “Bypass Transition Modeling: A New Method Which Accounts for Freestream Turbulence Intensity and Length Scale,” ASME Report No. 2000-GT-278.

Sharma, O. P., Renaud, E., Butler, T. L., Milsaps, K., Dring, R. P., and Joslyn, H. D., 1988, “Rotor-Stator Interaction in Multi-Stage Axial-Flow Turbines,” AIAA Report No. 88–3013.

Ames, F. E., 1995, “Advanced k-epsilon Modeling of Heat Transfer,” NASA Contract Report No. 4679.

Van Fossen, G. J., Simoneau, R. J., and Ching, C. Y., 1994, “Influence of Turbulence Parameters, Reynolds Number, and Body Shape on Stagnation-Region Heat Transfer,” NASA Technical Report No. 3487.

Arts, T., de Rouvroit, L. M., and Rutherford, A. W., 1990, “Aero-Thermal Investigation of a Highly Loaded Transonic Linear Turbine Guide Vane Cascade,” von Karman Institute for Fluids Dynamics Technical Note No. 174.

Schmidt, R. C., and Patankar, S. V., 1988, “Two-Equation Low-Reynolds-Number Turbulence Modeling of Transitional Boundary Layer Flows Characteristic of Gas Turbine Blades,” NASA Contract Report No. 4145.

Praisner, T. J., Clark, J. P., Grover, E. A., Bertuccioli, L., and Zhang, D., 2004, “Challenges in Predicting Component Efficiencies in Turbines with Low Reynolds Number Blading,” NASA/TM-2004-212913, p. 58

Blair, M. F., and Werle, M. J., 1981, “Combined Influence of Freestream Turbulence and Favorable Pressure Gradients on Boundary Layer Transition and Heat Transfer,” UTRC Report No. R81–914388–17.

Emmons, H. W., 1951, “The Laminar Turbulent Transition in a Boundary Layer. Part 1,” J. Aeronaut. Sci., 18 , pp. 490–498.

Schubauer, G. B., and Klebanoff, P. S., 1955, “Contributions on the Mechanics of Boundary Layer Transition,” NASA TN Paper No. 3489.

Narasimha, R., 1957, “On the Distribution of Intermittency in the Transition Region of a Boundary Layer,” J. Aeronaut. Sci., 24 , pp. 711–712.

Clark, J. P., Jones, T. V., and LaGraff, J. E., 1994, “On the Propagation of Naturally-Occurring Turbulent Spots,” J. Eng. Math., 28 , pp. 1–19.

Gostelow, J. P., Blunden, A. R., and Walker, G. J., 1994, “Effects of Freestream Turbulence and Adverse Pressure Gradients on Boundary-Layer Transition,” ASME J. Turbomach., 116 , pp. 392–404.

Halstead, D. E., Wisler, D. C., Okiishi., T. H., Walker, G. J., Hodson, H. P., and Shin, H. W., 1997, “Boundary Layer Development in Axial Compressors and Turbines: Part 3 of 4—LP Turbines,” ASME J. Turbomach., 119 , pp. 225–237.

Chen, K. K., and Thyson, N. A., 1971, “Extension of Emmons’ Theory to Flows on Blunt Bodies,” AIAA J., 9 (5), pp. 821–825.

Dey, J., and Narasimha, R., 1990, “Integral Method for the Calculation of Incompressible Two Dimensional Transitional Boundary Layers,” J. Aircr., 27 (10), pp. 859–865.

Solomon, W. J., Walker, G. J., and Gostelow, J. P., 1996, “Transition Length Prediction for Flows with Rapidly Changing Pressure Gradients,” ASME J. Turbomach., 118 , pp. 744–751.

Dhawan, S., and Narasimha, R., 1958, “Some Properties of Boundary Layer Flow During the Transition From Laminar to Turbulent Motion,” J. Fluid Mech.

[CrossRef], 3 , pp. 418–436.

Suzen, Y. B., and Huang, P. G., 2000, “Modeling of Flow Transition Using and Intermittency Transport Equation,” ASME J. Fluids Eng.

[CrossRef], 122 , pp. 273–284.

Steelant, J., and Dick, E., 2001, “Modeling of Laminar-Turbulent Transition for High Free Stream Turbulence,” ASME J. Fluids Eng.

[CrossRef], 123 , pp. 22–30.

Drela, M., 1995, “MISES Implementation of Modified Abu-Ghannam-Shaw Transition Criterion,” MIT Technical Report.

Gier, J., Ardey, S., and Heisler, A., 2000, “Analysis of Complex Three-Dimensional Flow in a Three-Stage LP Turbine by Means of Transitional Navier-Stokes Simulation,” ASME Paper No. 2000-GT-645.

Thermann, H., Mueller, M., and Niehuis, R., 2001, “Numerical Simulation of Boundary Layer Transition in Turbomachinery Flows,” ASME Paper No. 2001-GT-0475.

Roux, J., Lefebvre, M., and Liamis, N., 2002, “Unsteady and Calming Effects Investigation on a Very High Lift LP Turbine Blade—Part II: Numerical Analysis,” ASME Paper No. GT2002–30228.

Roberts, S. K., and Yaras, M. I., 2003, “Measurements and Prediction of Freestream Turbulence and Pressure-Gradient Effects on Attached-Flow Boundary-Layer Transition,” ASME Paper No. GT2003–38261.

Narasimha, R., 1985, “The Laminar Turbulent Transition Zone in the Boundary Layer,” Prog. Aerosp. Sci.

[CrossRef], 22 , pp. 29–80.

Fraser, C. J., Higazy, M. G., and Milne, J. S., 1994, “End-Stage Boundary Layer Transition Models for Engineering Calculations,” Proc. Inst. Mech. Eng., Part C: J. Mech. Eng. Sci., 208 (C1), pp. 47–58.

Narasimha, R., 1990, “Modeling the Transitional Boundary Layer,” NASA CR 187487.

Narasimha, R., 1991, “Recent Advances in the Dynamics of the Transition Zone,” ISABE Report No. 91 7006.

Owen, F. K., 1970, “Transition Experiments on a Flat Plate at Subsonic and Supersonic Speeds,” AIAA J., 8 (3), pp. 518–523.

Sharma, O. P., Wells, R. A., Schlinker, R. H., and Bailey, D. A., 1982, “Boundary Layer Development on Airfoil Suction Surfaces,” ASME J. Eng. Power, 104 , pp. 698–706.

Clark, J. P., 1993, “A Study of Turbulent-Spot Propagation in Turbine-Representative Flows,” D. Phil, University of Oxford, Oxford, England.

Narasimha, R., 2003, “Review of Recent Research in Bangalore on the Transition Zone,” NASA/TM-2004-212913, p. 63.

Hofeldt, A. J., 1996, “An Investigation of Naturally-Ocurring Turbulent Spots Using Thin-Film Gages,” Ph.D. thesis, University of Oxford, Oxford, England.

Tani, I., 1969, “Boundary-Layer Transition,” Annu. Rev. Fluid Mech.

[CrossRef], 1 , pp. 169–196.

Reshotko, E., 1976, “Boundary Layer Stability and Transition,” Annu. Rev. Fluid Mech.

[CrossRef], 8 , pp. 311–349.

Liepmann, H. W., 1945, “Investigation of Boundary Layer Transition on Concave Walls,” NACA Wartime Report No. W-87 (also NACA ACR 4J28).

Liepmann, H. W., 1943, “Investigations of Laminar Boundary Layer Stability and Transition on Curved Boundaries,” NACA Wartime Report No. W-107 (also NACA ACR 3H30).

Van Driest, E. R., and Blumer, C. B., 1963, “Boundary Layer Transition: Free Stream Turbulence and Pressure Gradient Effects,” AIAA J., 1 , pp. 1303–1306.

Mayle, R. E., and Schulz, A., 1997, “The Path to Predicting Bypass Transition,” ASME J. Turbomach., 119 , pp. 405–411.

Suder, K. L., O’Brien, J. E., and Reshotko, E., 1988, “Experimental Study of Bypass Transition in a Boundary Layer,” NASA TM Report No. 100913.

Kim, J., Simon, T. W., and Kestoras, M., 1994, “Fluid Mechanics and Heat Transfer Measurements in Transitional Boundary Layers Conditionally Sampled on Intermittency,” ASME J. Turbomach., 116 , pp. 405–416.

Morkovin, M. V., 1978, “Instability, Transition to Turbulence, and Predictability,” NATO AGARDograph No. 236.

Massey, B. S., 1986, "*Measures in Science and Engineering*", Ellis-Horwood, Ltd., Chichester, UK, pp. 125–127.

Michelassi, V., Rodi, W., and Giess, P.-A., 1998, “Experimental and Numerical Investigation of Boundary-Layer and Wake Development in a Transonic Turbine Cascade,” Aerosp. Sci. Technol., 3 , pp. 191–204.

White, F. M., 1991, "*Viscous Fluid Flow*", 2nd ed., McGraw-Hill, New York, pp. 273–274.

Schlichting, H., 1979, "*Boundary Layer Theory*", 7th ed., McGraw-Hill, New York, pp. 90–91, 470 .

Hofeldt, A. J., Clark, J. P., LaGraff, J. E., and Jones, T. V., 1998, “The Becalmed Region in Turbulent Spots,” NASA CP 1998–206958, pp. 95–98.

Herbert, T., 1988, “Secondary Instability of Boundary Layers,” Annu. Rev. Fluid Mech., 20 , pp. 487–526.

Walker, G. J., and Gostelow, J. P., 1990, “Effects of Adverse Pressure Gradients on the Nature and Length of Boundary-Layer Transition,” ASME J. Turbomach., 112 , pp. 196–205.

Mack, L. M., 1975, “Linear Stability Theory and the Problem of Supersonic Boundary Layer Transition,” AIAA J., 13 (3), pp. 278–289.

Volino, R. J., 2002, “Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions—Part 1: Mean flow and Turbulence Statistics,” ASME Paper No. 2002-GT-30236.

Volino, R. J., 2002b, “Separated Flow Transition Under Simulated Low-Pressure Turbine Airfoil Conditions: Part 2—Turbulence Spectra,” ASME Paper No. 2002-GT-30237.

Roberts, W. B., 1980, “Calculation of Laminar Separation Bubbles and Their Effect on Airfoil Performance,” AIAA J., 18 (1), pp. 25–31.

Walker, G. J., 1989, “Modeling of Transitional Flow in Laminar Separation Bubbles,” "*Proceedings of the Ninth International Symposium on Air Breathing Engines*", pp. 539–548.

Hatman, A., and Wang, T., 1999, “A Prediction Model for Separated Flow Transition,” ASME J. Turbomach., 121 , pp. 594–602.

Houtermans, R., Coton, T., and Arts, T., 2003, “Aerodynamic Performance of a Very High Lift LP Turbine Blade With Emphasis on Separation Prediction,” ASME Paper No. 2003-GT-38802.

Davis, R. L., Carter, J. E., and Reshotko, E., 1985, “Analysis of Transitional Separation Bubbles on Infinite Swept Wings,” AIAA Paper No. 85–1685.

Bons, J. P., Hansen, L. C., Clark, J. P., Koch, P. J., and Sondergaard, R., 2005, “Designing Low-Pressure Turbine Blades With Integrated Flow Control,” ASME Paper No. GT2005–68962.

Lou, W., and Hourmouziadis, J., 2000, “Separation Bubbles Under Steady and Periodic-Unsteady Main Flow Conditions,” ASME Paper No. 2000-GT-0270.

Walker, G. J., Subroto, P. H., and Platzer, M. F., 1988, “Transition Modeling Effects on Viscous/Inviscid Interaction Analysis of Low Reynolds Number Airfoil Flows Involving Laminar Separation Bubbles,” ASME Paper No. 88-GT-32.

Praisner, T. J., Grover, E. A., Rice, M. J., and Clark, J. P., 2004, “Predicting Transition in Turbomachinery, Part II—Model Validation and Benchmarking,” ASME Paper No. GT-2004–54109.